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Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air / / William I. Scallion
| Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air / / William I. Scallion |
| Autore | Scallion William I. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 1999 |
| Descrizione fisica | 1 online resource (54 pages) : illustrations |
| Collana | NASA TM- |
| Soggetto topico |
Controllability
Effectiveness Lifting bodies Scale models Wind tunnel tests Elevons |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706169003321 |
Scallion William I.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 1999 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Space shuttle orbiter trimmed center-of-gravity extension study : summary report / / William I. Scallion and W. Pelham Phillips
| Space shuttle orbiter trimmed center-of-gravity extension study : summary report / / William I. Scallion and W. Pelham Phillips |
| Autore | Scallion William I. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , 1985 |
| Descrizione fisica | 1 online resource (50 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Center of gravity
Aerodynamic configurations Space Shuttle orbiters Wind tunnel tests Design analysis Space shuttles - Design and construction Center of mass Space vehicles - Aerodynamics |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Space shuttle orbiter trimmed center-of-gravity extension study |
| Record Nr. | UNINA-9910709630903321 |
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Scallion William I.
|
||
| Washington, D.C. : , : National Aeronautics and Space Administration, , 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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